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Document Type:会议论文
Community:高温气体动力学国家重点实验室
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A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels
会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
Authors:
Jin YC(靳一超)
;
Wu K(吴坤)
;
Lu Y(陆阳)
;
Fan XJ(范学军)
Adobe PDF(1121Kb)
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Submit date:2022/07/04
Temperature and H2O concentration measurements for a hybrid rocket motor plume using a single mid-infrared tunable diode laser
会议论文
2020 Applied Optics and Photonics China: Optical Sensing and Imaging Technology, AOPC 2020, Xiamen, PEOPLES R CHINA, 25 August 2020 through 27 August 2020
Authors:
Fang SH(方思晗)
;
Wang ZZ(王泽众)
;
Li RJ(李仁杰)
;
Zhang ZL(张泽林)
;
Lin X(林鑫)
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(1569Kb)
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Submit date:2021/06/11
concentration
hybrid rocket motor
nozzle exit
temperature
Tunable diode laser absorption spectroscopy (TDLAS)
water vapor
Validation and application of gas radiation computation at earth re-entry conditions
会议论文
31st International Symposium on Rarefied Gas Dynamics, RGD 2018, University of StrathclydeGlasgow; United Kingdom;, 23 July 2018 ~ 27 July 2018
Authors:
Lyu JM
;
Cheng XL
;
Yu JJ
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(2168Kb)
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Submit date:2020/11/20
Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor
会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:
Yao W(姚卫)
;
Li B(李波)
Adobe PDF(1665Kb)
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Submit date:2020/11/20
Dynamic zone flamelet model
GH2/GO2
Large Eddy Simulation (LES)
Rocket combustor
Turbulence-chemistry interaction
Supercritical GN2/GH2 jet modeled by the ECS method
会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:
Yao W(姚卫)
;
Jin YC(靳一超)
;
Lee YC(李亚超)
Adobe PDF(1048Kb)
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Submit date:2020/11/20
Ventilated partial cavitating flow around a blunt body near the free surface
会议论文
16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2016, Honolulu, HI, United states, April 10, 2016 - April 15, 2016
Authors:
Wang YW(王一伟)
;
Wu XC(吴小翠)
;
Huang CG(黄晨光)
Adobe PDF(757Kb)
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View/Download:193/40
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Submit date:2019/11/20
Axisymmetric bodies
Cavity boundaries
Free surfaces
High
speed underwater vehicles
Launching systems
Media properties
Unsteady behaviors
Ventilated cavitation
Optimization of the self-condensing CO2 transcritical power cycle using solar thermal energy
会议论文
10th International Conference on Applied Energy (ICAE), Hong Kong, HONG KONG, AUG 22-25, 2018
Authors:
Pan LS(潘利生)
;
Li,Bing
;
Shi,Weixiu
;
Wei XL(魏小林)
Adobe PDF(1140Kb)
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Submit date:2022/11/24
CO2 transcritical power cycle
Supercritical CO2 Brayton cycle
Solar thermal energy
CO2 condensation
Influence of Chemical Mechanisms on Supersonic Combustion Characteristics Fueled by Kerosene
会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio, July 9-11, 2018
Authors:
Yao W(姚卫)
;
Wu K(吴坤)
;
Lee YC(李亚超)
;
Fan XJ(范学军)
Adobe PDF(1156Kb)
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View/Download:430/0
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Submit date:2018/12/26
Real-gas Effect Accounted for by the Principle of Extended Corresponding States in Modeling Supersonic Kerosene Jet
会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
Authors:
Wang Y
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2018/12/26
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
Adobe PDF(1249Kb)
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Submit date:2018/01/16
Combustion
Diesel Engines
Hydrogen
Large Eddy Simulation
Spacecraft
Stabilization
Supersonic Aircraft
Temperature Measurement
Wall Flow